View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 57851U 26145.39096685 +.00000000 +00000-0 +60769-4 0 00005
2 57851 53.1613 287.6380 0001125 80.7216 279.3913 15.31701334 06
| Epoch (UTC): | 25 May 2026 09:22:59 |
| Eccentricity: | 0.0001125 |
| inclination: | 53.1613° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 287.6380° |
| argument of perigee: | 80.7216° |
| revolutions per day: | 15.31701334 |
| mean anomaly at epoch: | 279.3913° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|